N14645
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
28 reports on file, 1998-07-16 – 2011-04-19.
Part: MEC — FAULTY (NR 2 ENGINE) · airframe 35,500 hrs · 18,812 cycles
REJECTED TAKEOFF AT 85 KTS DUE TO THE NR 2 N1 GAUGE BEING VERY SLOW TO REACT AND NOT READING ABOVE 60 PERCENT N1. THE NR 2 THROTTLE WAS ALSO SLOW TO REACT BUT DID MATCH THE N1 THROTTLE. REF. N/R 4484876, 4457301 FOR CORRECTIVE ACTION. REMOVED AND REPLACED MEC NR 2 ENGINE PER AMM 73-21-01. VBV AND VSV FEEDBACK CABLE TESTS CHECK GOOD. SEE N/R 4484876 FOR LEAK AND OPS CHECK.
Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 34,924 hrs · 18,520 cycles
AC WOULD NOT PRESSURIZE IN AUTO OR STANDBY. T/S PER MM 21-31-00. NR 2 AUTO PRESSURE CONTROLLER FAILED. REMOVED AND REPLACED DAPC AND OPS CHECKED AS PER MM 21-31-21. COMPLIED WITH EC 2100-01187. PER MM 21-30-00-800-801C3. LMPH CHECK. ALL REQUIREMENTS OF ECRA SATISFIED ABOVE MINIMUM REQUIREMENT.
Earlier reports · 1998–2008 · 26 reports
2008
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,433 hrs · 15,165 cycles
BODY STATION 360 LEFT BETWEEN S-8 AND S-9 IS CRACKED. INSTALLED INTERIM REPAIR AT CABIN FRAME BODY STATION 360 LEFT BETWEEN S-8L AND S-9L PER ECRA 5310-04782 DIP CONTROL NUMBER 88780 FOR FRAME REPAIR AT BODY STATION 360 S-8L AND S-9L AT PASSENGER SERVICE UNIT (PSU) BRACKET ACCOMPLISH A PERMANENT REPAIR BEFORE 10 JUNE 09 PER ECRA 5310-04782 PART 3.
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,433 hrs · 15,165 cycles
BODY STATION 827 RIGHT BETWEEN S-8R AND S-9R IS CRACKED. INSTALLED INTERIM REPAIR AT CABIN FRAME BODY STATION 827 RIGHT BETWEEN S-8R AND S-9R PER ECRA 5310-04783 DIP CONTROL NUMBER 88782 FOR FRAME REPAIR AT BODY STATION 827 S-8R AND S-9R AT PASSENGER SERVICE UNIT (PSU) BRACKET ACCOMPLISH A PERMANENT REPAIR BEFORE 09 JUNE 09 PER ECRA 5310-04783 PART 3.
Part: SKIN — CRACKED (L/E SLAT) · airframe 28,433 hrs · 15,165 cycles
NUMBER 2 SLAT HAS CRACKS ON THE LOWER TRAILING EDGE AT AFT RIVETS FSS 454. TRIMMED OUT CRACKED SKIN AND INSTALLED REPAIR DOUBLER AND FILLER PER SRM 57-43-01, FIG 201 AND REINSTALLED INNER PANEL PER SRM 51-40-02.
Part: SKIN — CRACKED (L/E SLAT) · airframe 28,433 hrs · 15,165 cycles
NUMBER 2 SLAT HAS CRACKS ON THE LOWER TRAILING EDGE AT AFT RIVETS FSS 424 AND 426. TRIMMED OUT CRACKED SKIN AND INSTALLED REPAIR DOUBLER AND FILLER PER SRM 57-43-01 FIG 201 AND REINSTALLED INNER PANEL PER SRM 51-40-02.
Part: SKIN — WORN (FUSELAGE) · airframe 28,433 hrs · 15,165 cycles
FUSELAGE UPPER SKIN IS WORN AT STATION 874-882 RBL-3 TO RBL-4 FROM DORSIL FIN SEAL. BLENDED OUT AREA AND INSTALLED DOUBLER, TRIPLER AND WEAR STRIPS REFINISHED AREA PER SRM 53-60-01, REPAIR 10, PROCEDURE III.
Part: SKIN — WORN (FUSELAGE) · airframe 28,433 hrs · 15,165 cycles
UPPER FUSELAGE SKIN IS WORN AT STATION 864-882 LBL-1 TO LBL-4 FROM DORSAL FIN SEAL. BLENDED OUT AREA AND INSTALLED DOUBLER, TRIPLER AND WEAR STRIPS REFINISHED AREA PER SRM 53-60-01 REPAIR 10, PROCEDURE III.
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,433 hrs · 15,165 cycles
BODY STATION 787 LEFT-HAND CRACKED AT AIR GRILL MOUNT BRACKET. INSTALLED FRAME REPAIR PER EA 5310-04498.
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,433 hrs · 15,165 cycles
BODY STATION 747 LEFT CRACKED AT AIR GRILL MOUNT. INSTALLED REPAIR ANGLES AND COLD WORKED 6EA HOLES PER EA 5310-04498 OP 02.
Part: SKIN — DENTED (CARGO DOOR) · airframe 28,433 hrs · 15,165 cycles
NUMBER 2 CARGO DOOR EXTERIOR SKIN DENTED 12 INCHES FROM AFT EDGE AND 15 INCHES FROM THE TOP. CUT OUT DENT, FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 52-00-01 FIGURE 201 REPAIR 3.
Part: SKIN — DENTED (CARGO DOOR) · airframe 28,433 hrs · 15,165 cycles
NUMBER 2 CARGO DOOR EXTERIOR SKIN DENTED 21 INCHES FROM AFT EDGE AND 15 INCHES FROM THE TOP. CUT OUT DENT, FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 52-00-01 FIGURE 201 REPAIR 3.
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,433 hrs · 15,165 cycles
BODY STATION 907 LEFT CRACKED AT AIR GRILL MOUNT. INSTALLED REPAIR ANGLES AND COLD WORKED 6EA HOLES PER EA 5310-04498 OP 02.
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,433 hrs · 15,165 cycles
STATION 727B LEFT BETWEEN S8L AND S9L IS CRACKED. REPAIRED CRACK PER EA 5310-04498.
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,433 hrs · 15,165 cycles
STATION 440 BETWEEN S8R & S9R IS CRACKED. REPAIRED CRACK AT STATION 440 BETWEEN S8R AND S9R PER EA 5310-04498.
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,433 hrs · 15,165 cycles
STATION 747 BETWEEN S8R & S9R IS CRACKED. INSTALLED REPAIR DOUBLERS AND COLD WORKED 6 EA HOLES PER EA 5310-04498 OP 02.
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,433 hrs · 15,165 cycles
STATION 400 LT BETWEEN S8L AND S9L IS CRACKED. REMOVED AND INSTALLED NEW REPAIR ANGLES A AND B PER EA 5310-04498 OP2.
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,433 hrs · 15,165 cycles
BS 380 BETWEEN S8R & S9R IS CRACKED. REPAIRED CRACK PER EA 5310-04498.
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,433 hrs · 15,165 cycles
BODY STATION 727B RIGHT BETWEEN S8 AND S9 IS CRACKED. REMOVED DAMAGED SECTION OF FRAME, FABRICATED, TREATED, PRIMED AND INSTALLED REPAIR PIECES PER EA 5310-04498.
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,433 hrs · 15,165 cycles
STATION 400 BETWEEN S8R & S9R IS CRACKED. REPAIRED CRACK AT STATION 400 BETWEEN S8R AND S9R PER EA 5310-04498.
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,433 hrs · 15,165 cycles
RIGHT FRAME IS CRACKED AT S8R STATION 787. REPAIRED FRAME AT S8R STATION 787 PER EA 5310-04498.
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,433 hrs · 15,165 cycles
RIGHT FRAME IS CRACKED AT S8R STATION 907. REPAIRED FRAME AT S8R STATION 907 PER EA 5310-04498.
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,433 hrs · 15,165 cycles
RIGHT FRAME IS CRACKED AT S8R STATION 867. REPAIRED FRAME AT S8R STATION 867 PER EA 5310-04498.
2003
Part: BUSHING — CORRODED (HORIZ STAB) · airframe 16,565 hrs · 8,880 cycles
INSPECTION FOUND RT HORIZONTAL STABILIZER CENTER SECTION FRONT SPAR LOWER FORWARD LUG PITTED AT BUSHING. THE BUSHING WAS REMOVED AND REPLACED IAW CMM 55-10-06.
Part: BUSHING — CORRODED (HORIZ STAB) · airframe 16,565 hrs · 8,880 cycles
INSPECTION FOUND LT HORIZONTAL STABILIZER CENTER FORWARD SPAR LOWER AFT LUG PITTED AT BUSHING. A NEW BUSHING WAS INSTALLED IAW CMM 55-10-06.
Part: ANGLE — GOUGED (FUSELAGE) · airframe 16,565 hrs · 8,880 cycles
INSPECTION FOUND LT VERTICAL STABILIZER PANEL ATTACH ANGLE GOUGED AT STA 1065-1085 JUST BELOW VERTICAL STAB ON LT SIDE JUST FORWARD OF RUDDER. THE ATTACH ANGLE WAS REMOVED AND REPLACED IAW ECRA 55380-01013.
1998
Part: CYLINDER — INOPERATIVE (NLG)
WHEN LANDING GEAR WAS LOWERED ON APPROACH, THE NOSE GEAR APPEARED TO HANG UP FOR SEVERAL SECONDS AND THEN SLAMMED DOWN HARD. THREE GREEN GEAR LIGHTS WERE INDICATED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NOSE GEAR TRANSFER CYLINDER AT FAULT. THE NLG TRANSFER CYLINDER WAS REMOVED AND REPLACED IAW MM 32-33-41. THE GEAR WAS SWUNG SEVERAL TIMES WITH OPERATION CHECKING GOOD AND NO LEAKS WERE NOTED.
Part: ACTUATOR — INOPERATIVE (NLG)
WHEN LANDING GEAR WAS EXTENDED ON APPROACH TO IAH, THE NOSE GEAR GAVE A HARD LOUD THUD THAT COULD BE FELT ON AIRCRAFT FLOOR. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NLG RETRACT ACTUATOR AT FAULT. THE ACTUATOR WAS REMOVED AND REPLACED IAW MM 32-33-11. LEAK AND OPERATIONAL CHECKS WERE GOOD.